IPET I11
Integrated I11 motor 14S FOC 70A ESC and folding I42 propeller system for 40–48 kg quadcopter UAVs requiring heavy lift endurance strong thrust reserve and stable professional payload operation
Engineering Fit Check
Use these core parameters for initial airframe compatibility review Final sizing should also consider altitude ambient temperature payload distribution mission duty cycle propeller clearance and the thrust reserve required by the flight control strategy
Integrated by Design Validated as a System
Motor ESC and matched propeller are engineered as one propulsion architecture to reduce integration work improve system consistency and provide a validated starting point for UAV platform development
Motor and ESC Integration
A compact integrated architecture reduces external wiring connector count and installation complexity while supporting more consistent electrical control and thermal behavior
Matched Propeller Setup
Propeller sizing is selected around the motor and ESC operating range to balance thrust efficiency current draw and thermal load at system level
Faster Platform Integration
A defined propulsion configuration reduces component sourcing compatibility testing and repeated tuning during prototype development
System Level Performance Data
Thrust efficiency current RPM and temperature are evaluated as a complete propulsion system to support airframe selection and validation
Engineered for Heavy Lift Endurance at Scale
Designed for 40–48 kg quadcopter UAVs that need efficient heavy lift operation large propeller integration long service life and dependable thermal management under high power loads
High Efficiency at the Heavy Lift Operating Point
The validated I11 configuration delivers approximately 10.0 g/W at 10.0 kg thrust helping large UAV platforms manage energy demand around a practical heavy lift operating point
Folding I42 Propeller for Large Airframes
The folding 42 inch propeller provides the disk area required for efficient heavy lift propulsion while reducing the storage and transportation footprint of large UAV platforms
Long Life Protection and Wide Temperature Reliability
Core components are developed around a 10,000 hour service life target while IP46 protection and a recommended ambient temperature range from −30°C to 65°C support repeated heavy lift missions involving dust moisture cold starts and high ambient temperatures
High Capacity Thermal Management for Heavy Lift Operation
The motor and 70A FOC ESC thermal architecture is sized for sustained high power operation helping control temperature rise and maintain stable propulsion output under heavy loads
Where I11 Fits Best
Designed for 40–48 kg quadcopter UAVs that need heavy lift endurance strong payload support and dependable propulsion integration for large professional platforms
Heavy-Lift Logistics
Supports high-payload cargo transport and resupply missions where large multirotor platforms require dependable lift capacity and efficient propulsion
Large-Scale Surveying
Supports larger LiDAR, photogrammetry, and multi-sensor payloads for large-scale survey missions requiring stable lift and longer productive flight time
Multi-Sensor Offshore Inspection
Supports EO/IR, LiDAR, gas detection, and other professional payloads for complex offshore inspection missions requiring greater lift capacity and stable flight
